Boeing 727-228

Service difficulty reports · 1,323

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duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '727228'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR DHL96721108Skin · crackedAT C-CHECK, TOP COVE PANEL FWD OF NR 9 SPOILER CENTER SKIN IS CRACKED AND BROKEN. STOP DRILLED CRACK, INSTALLED DOUBLER REPAIR PER SRM 51-40-2, 3 BY 4 PER SRM 51-40-2.Jun 5, 1996 · N721DH · Boeing 727228 · Wing, Plate/SkinSDR DHL96721101Frame · crackedAT C-CHECK, BAGGAGE FRAME CRACKED AND CORRODED AT STA 1166 BETWEEN STR 29 AND 30 RT. CUT OUT DAMAGED AREA 2 BY 4 AND INSTALLED REPAIR PER SRM 53-10-4, 9 BY 8.Jun 5, 1996 · N721DH · Boeing 727228 · Fuselage Main, FrameSDR DHL9672104CSkin · crackedAT C-CHECK, FOUND EXTERIOR FUSELAGE WITH CRACK AT BS 227.8 WL 223 AND BS 235.8 AT WL 230 LEFT SIDE. INSTALLED DOUBLER REPAIR PER SRM 53-20-3, REPAIR 15 BY 18.5.Jun 5, 1996 · N721DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR 96DHL72190CStringer · dentedAT C-CHECK, SMALL DENTS AT FUS STA 300 STR 14, 15, RT. REPAIRED STRINGER AT STA 14 PER SRM 53-10-3, 18.Jun 5, 1996 · N721DH · Boeing 727228 · Fuselage Main, Longeron/StringerSDR 96DHL72187CFrame · crackedAT C-CHECK, BS 760.95 RT SIDE FRAME CRACKED THROUGH INBD FLANGE EXTENDING OUTBD TO OUTER FLANGE. INSTALLED REPAIR KIT ON CABIN FRAME AT FS 760.95 PER S/B 53-197.Jun 5, 1996 · N721DH · Boeing 727228 · Fuselage Main, FrameSDR DHL9672182CFitting · crackedAT C-CHECK, FOUND CORROSION S-8L END FITTING AT 740. REMOVED CORROSION, FOUND CRACKED END FITTING. REPLACED FITTING PER SRM 51-10-1.Jun 4, 1996 · N721DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR DHL96721107Panel · delaminatedAT C-CHECK, LEFT WING UPPER SURFACE PANEL 8147, HAS DELAMINATION AND SURFACE CORROSION. INSTALLED BONDING REPAIR PER SRM 51-40-5 AND 51-40-6, 40 BY 20 AND INSTALLED PANEL PER SRM 51-30-2.Jun 4, 1996 · N721DH · Boeing 727228 · Wing, Plate/SkinSDR DHL96721105Rib · crackedAT C-CHECK, FOUND LEFT WING L/E SKIN SUPPORT RIB CRACKED ON INBD SIDE OF NR 3 LEADING EDGE FLAP WELL ON INBD SIDE, APPROX 18. REMOVED SUPPORT RIB AND INSTALLED NWE RIB PER SRM 51-10-1.Jun 4, 1996 · N721DH · Boeing 727228 · Wing, Rib/BulkheadSDR 96DHL72185CSkin · corrodedAT C-CHECK, FOUND BULGING UNDER RAIN GUTTER AT BOTH SIDES OF SEAM STA 1430 WL 259 EXT RT SIDE. CUT OUT DAMAGED SKIN, FABRICATED FILLER 3 BY 4 FT, DOUBLER 6 BY 3 FT; FILLER 2 BY 3 FT AND DOUBLER 4 BY 6, INSTALLED PER SRM 55-30-3.Jun 4, 1996 · N721DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR 96DHL721109Panel · delaminatedAT C-CHECK, RT UPPER WING APU EXHAUST FIBERGLASS PANEL IS DELAMINATED ON OUTBD SIDE. INSTALLED BONDING REPAIR PER SRM 51-40-6, 65 BY 27.25.Jun 4, 1996 · N721DH · Boeing 727228 · Wing, Plate/SkinSDR DHL9672186CBulkhead · crackedAT C-CHECK, BS 178 BULKHEAD WEB CRACKED AT RIVET WL 196 BL 2 RT. STOP DRILLED CRACKS, INSTALLED WEB REPAIR 5 BY 5 PER SRM 51-40-2.Jun 3, 1996 · N721DH · Boeing 727228 · Fuselage Main, BulkheadSDR DHL9672175CAngle · crackedAT C-CHECK, ATTACH ANGLE CRACKED AT BS 900 LBL 65 OUTBD SIDE OF PRESSURE DECK, 12 BELOW PRESS DECK. REPLACED ATTACH ANGLE 4 BY 6 PER SRM 51-10-1.Jun 3, 1996 · N721DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR DHL9672117CPressure Deck · crackedAT C-CHECK, FOUND NOSE W/W PRESSURE DECK CRACKED AT STA 280. FABRICATED AND INSTALLED DOUBLER 19 BY 10 PER SRM 51-40-2.Jun 3, 1996 · N721DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR DHL96721115Angle · corrodedAT C-CHECK, CORROSION FOUND UNDER FS 950 CASTING SPLICE PLATE ON LEFT W/W AFT WALL 16 BELOW SIDE STRUT AFT BEARING HOUSING. REMOVED CORRODED SPLICE ANGLE, CUT OUT CORRODED WEB, INSTALLED WEB REPAIR PER SRM 51-40-2, 9 BY 3.5. REPLACED SPLICE PLATE ANGLE, INSTJun 3, 1996 · N721DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR DHL96721100Floorbeam · corrodedAT C-CHECK, CABIN FLOORBEAM BS 328 LBL 30 IS CORRODED AT FLOORBEAM SUPPORT ANGLE ATTACH POINTS. INSTALLLED ANGLE REPAIRS 17 BY 1.5 BY 1.5, 15.25 BY 1.5 BY 1.5 PER SRM 51-40-4.Jun 1, 1996 · N721DH · Boeing 727228 · Fuselage Main, Floor BeamSDR DHL96721116Forging · crackedVERTICAL FIN FRONT SPAR FORGING HAS INTERIM REPAIR PER AVITAS EO 96PMS I114RO-1. REMOVED INTERM REPAIR PER SRM 51-30-2, INSTALLED VERTICAL FIN FRONT SPAR FORGING PER AVITALS ENGINEERING DRAWING 96PMSI124D-1.May 31, 1996 · N721DH · Boeing 727228 · Vertical StabilizerSDR DHL9672108CAttach · crackedAT C-CHECK, FOUND NR 7 SLAT ACTUATOR ROD END ATTACH IN OUTBD RIB IN SLAT CRACKED. STOP DRILLED CRACK, INSTALLED REPAIR PER SRM 57-50-3, REPAIR 5 BY 4 BY .5.May 5, 1996 · N721DH · Boeing 727228 · Leading Edge DevicesSDR DHL9672103CSkin · crackedAT C-CHECK, EXTERIOR FUSELAGE HAS 2 CRACKS AROUND FASTENERS AT BS 188 WL 224 AND WL 219, BS 196 AND WL 222 LEFT SIDE. CUT OUT DAMAGE, INSTALLED DOUBLER 15 BY 18.5 PER SRM 53-30-3.May 5, 1996 · N721DH · Boeing 727228 · Fuselage Main, Plate/SkinSDR DHL96720001Controller · malfunctionedL1 WINDOW HEAT AMBER OVERHEAT LIGHT ON ZERO DEGREES, RESET 14 MINUTES TO OVERHEAT AGAIN. FOUND A LOOSE SPARE SENSOR TERMINAL END. REPLACED SAME, CHECKED L1 WINDOW RESISTANCE AND TAP SETTING. VOLTAGE WAS WITHIN LIMITS. REPLACED HEAT CONTROLLER FOR PRECAUTIOApr 27, 1996 · N720DH · Boeing 727228 · Windshield/Door Rain/Ice RemovalSDR 96DHL72601CFloor Beam · corrosionAT C-CHECK, FOUND CABIN FLOOR BEAM AT STA 480 SURFACE HAS MORE THAN 20 PERCENT OF MATERIAL REMOVED DUE TO CORROSION. CUT OUT SECTION OF FLOOR BEAM, INSTALLED REPAIR RBL ZERO TO RBL 32 PER SRM 53-10-8.Apr 10, 1996 · N726DH · Boeing 727228 · Fuselage Main, Floor BeamSDR 96DHL7219A1Forging · crackedAFT AIRSTAIRS VERTICAL FIN FRONT SPAR FORGING APPROX FS 1195 HAS CRACK INDICATIONS IN RADIUS OF LOWER FLANGE EXTENDING APPROX 3 INCHES TO THE RIGHT OF SPLICE PLATE AT 6 O'CLOCK. STOP DRILLED CRACK. HFEC INSPECTION CONFIRMED CRACK ENDS AT STOP HOLE. FABRICATMar 12, 1996 · N721DH · Boeing 727228 · Fuselage, Stabilizer Attach FittingsSDR DHL96721001Switch · malfunctionedAFTER GEAR RETRACTION AT PAP ALL 3 GEAR SHOWED RED AND GREEN LIGHTS ILLUMINATED ON FORWARD PANEL, DOOR LIGHTS WERE NOT ILLUMINATED. ON S/O PANEL SECONDARY MAIN GEAR LIGHTS WERE ILLUMINATED, TAIL SKID LIGHT WAS ILLUMINATED AND NO GEAR DOOR LIGHTS. CYCLED GEARFeb 26, 1996 · N721DH · Boeing 727228 · Landing Gear Position and WarningSDR DHL97724002Hyd Press Trans · leakingHYD BRAKE PRESSURE GAUGE INDICATES 1,500 LBS, 'A' AND 'B' HYD PRESSURE AND QUANTITY IS NORMAL. BRAKES WORKED NORMALLY ON LANDING. FOUND BRAKE ACC SHRADER VALVE LEAKING IN RT W/W. REPLACED VALVE, LEAK CHECKS GOOD. ALSO, FOUND BRAKE ACC PRESS TRANSMITTER LEAFeb 18, 1996 · N724DH · Boeing 727228 · Landing Gear Brake SystemSDR 96ZZZM502Skin · crackedDURING C-CHECK, FOUND CRACK RIGHT WING UPPER SKIN PANEL JUST FWD OF NR 10 SPOILER. STOP DRILL AT CRACK RT UPPER SKIN PANEL JUST FWD OF NR 10 SPOILER AS PER SRM 51-10-1. INSTALLED DOUBLER REPAIR AS PER SRM 51-40-2 7075-T6 .032 6 INCH BY 2.5 INCH LOT 133261 POFeb 3, 1996 · N724DH · Boeing 727228 · Wing, Plate/SkinSDR 96ZZZM501Rib · crackedDURING C-CHECK, FOUND RT WING LOWER FLANGE OF WING RIB CRACKED AT WS 629 AT LOWER STRINGER 8 PER PENETRANT INSPECTION PER SB 727-57-0127 REV 3 ENDS OF CRACK MARKED. STOP DRILLED CRACK PER SRM 51-10-1 AT WS 629 LOWER STRINGER 8 OF WING RIB. INSTALLED WING INSFeb 3, 1996 · N724DH · Boeing 727228 · Wing, Rib/BulkheadSDR 96ZZZM500Rib · crackedDURING C-CHECK, FOUND RIGHT WING LOWER FLANGE OF WING RIB CRACKED AT WS 686 AT STRINGER 8 TWO PARALLEL CRACKS AND AT STRINGER 6 AT PREVIOUS REPAIR. PENETRANT INSPECTION PER BOHM 20-20-2 PER SB 727-57-0127. ENDS OF CRACKS MARKED. REMOVED RT WING RIB AT WS 68Feb 3, 1996 · N724DH · Boeing 727228 · Wing, Rib/BulkheadSDR 96ZZZM499Rib · crackedDURING C-CHECK, FOUND STATION 601 WING RIB LOWER FLANGE HAS CRACKS AT NR 6 AND NR 8 STRINGER LOCATIONS. STOP DRILLED CRACKS AT NR 6 AND NR 8 STRINGER TO RIB LOCATION, ON RIB LOWER FLANGE STATION 601.5 PER SB 727-57-0127 FIG 2. NO CRACKS PROGRESSED AFTER STOPFeb 3, 1996 · N724DH · Boeing 727228 · Wing, Rib/BulkheadSDR 96ZZZM498Hat Channel · corrosionDURING C-CHECK, FOUND FORWARD LAVATORY THRESHOLD HAD LIGHT CORROSION AROUND CLIP NUTS ON HAT CHANNEL. REMOVED AND REPLACED HAT CHANNEL AS PER SRM 51-10-1 P4 AND SRM 51-30-2. P/N 60-357 7075-T6 PO NR 9600125 SIZE OF THE CHANNEL 40 INCH AT FWD LAVATORY AREA LOFeb 3, 1996 · N724DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR 96ZZZM497Door Frame · crackDURING C-CHECK, HFEC CRACK INDICATION AT NR 2 CARGO DOOR CUT OUT FWD FRAME WEB, JUST INBOARD OF LOWER FRAME DOOR STOP IN LINE WITH STRINGER 26R CRACK AND END OF CRACK. STOP DRILLED CRACK PER 51-10-1. INSTALLED WEB REPAIR PER SB 727-53-199R1 P 93110229 .080 7Feb 3, 1996 · N724DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR 96ZZZM496Skin · gougedDURING C-CHECK, FOUND MAIN CARGO DOOR EXTERIOR SKIN GOUGED AND SEPARATING ALSO, SEAL RETAINER TORN AT LOWER FORWARD CORNER OF MCD. REMOVED AND REPLACED AFT LOWER CORNER AT MAIN CARGO DOOR AS PER SRM 51-10-1 PAGE 4 2024-0 .025 12 INCH BY 3 INCH LOT NR 620352 PFeb 3, 1996 · N724DH · Boeing 727228 · Cargo/Baggage DoorsSDR 96ZZZM495Frame · crackedDURING C-CHECK, HFEC HAS INDICATED CRACKS TWO EACH STATION 870 JUST BELOW STRINGER 9 MAIN FRAME SPLICE OUTBOARD FLANGE, CRACKS LOCATED IN AFT ROW NR 4 BOTTOM HOLE IN MAIN FRAME AT 4 AND 5 O'CLOCK POSITION APPROX. REAMED HOLE TO NEXT SIZE .0156 AS PER SRM 51-3Feb 3, 1996 · N724DH · Boeing 727228 · Fuselage Main, FrameSDR 96ZZZM494Frame · crackedDURING C-CHECK, HFEC HAS INDICATED CRACKS ONE EACH STATION 870 JUST BELOW STRINGER 9R MAIN FRAME SPLICE OUTBOARD FLANGE, CRACKS LOCATED NEXT TO AFT ROW, ROW 3 NEXT TO BOTTOM HOLE (THIRD HOLE FROM TOP) AT ABOUT 11 O'CLOCK POSITION. REAMED HOLE TO NEXT SIZE .01Feb 3, 1996 · N724DH · Boeing 727228 · Fuselage Main, FrameSDR 96ZZZM493Fittings · crackedDURING C-CHECK, FOUND RIGHT ELEVATOR HINGE SUPPORT FITTINGS ARE CRACKED AT STATION 50.5 AND 66.5 AS SEEN THROUGH ACCESS PANELS ON BOTTOM SIDE OF ELEVATOR AS PER MM CHAP 27-50-5. INSTALLED THE REPLACEMENT ELEVATOR AS PER MM CHAP 27-30-5. INSTALLED ELEVATOR BAFeb 3, 1996 · N724DH · Boeing 727228 · Elevator StructureSDR 96ZZZM492'S' Duct Skin · corrodedDURING C-CHECK, FOUND NR 2 ENGINE 'S' DUCT INNER SKIN BULGED RIVET PULLED THROUGH 50 INCHES AFT OF SECOND ROW OF VORTEX GEN'S 6 O'CLOCK POSITION. CUT DAMAGED AREA 2 INCH BY 2 INCH PER SRM 54-10-3. INSTALLED CENTER ENGINE INTAKE DUCT SKIN DOUBLE REPAIR PER SRFeb 3, 1996 · N724DH · Boeing 727228 · Nacelle/Pylon, Plate/SkinSDR 96ZZZM491'S' Duct Skin · corrodedDURING C-CHECK, FOUND NR 2 ENGINES 'S' DUCT INNER SKIN BULGED RIVET PULLED THROUGH 8 INCHES AFT OF SECOND ROW OF VORTEX GEN'S 6 O'CLOCK POSITION. CUT OUT DAMAGED AREA SKIN PER SRM 54-10-3 FIG 10. INSTALLED DOUBLER REPAIR PER SRM 54-10-3 FIG 10 IN NR 2 ENGINEFeb 3, 1996 · N724DH · Boeing 727228 · Nacelle/Pylon, Plate/SkinSDR 96ZZZM490Rib · crackedDURING C-CHECK, FOUND LEFT WING, LOWER FLANGE OF WING RIB AT WS 686 CRACKED AT STRINGER 6 AND STRINGER 8. MARKED PENETRANT INSPECTION PER OHM 20-20-2 PER SB 727-57-0127. STOP DRILLED EACH END OF CRACKS AS PER SRM 51-10-1. INSTALLED WING RIB REPAIR AS PER SRFeb 3, 1996 · N724DH · Boeing 727228 · Wing, Rib/BulkheadSDR 96ZZZM489Rib · mis repairedDURING C-CHECK, FOUND WING RIB STATION 656 HAS PREVIOUS REPAIR WITH CUTOUT EXCEEDING 3 INCH LIMIT ON SRM 57-10-5 FIG 2. REMOVED AND REPLACED WING RIB AT STATION 656 PER SB 727-57-0127.Feb 3, 1996 · N724DH · Boeing 727228 · Wing, Rib/BulkheadSDR DHL727005Shutoff Valve · failedAIRCRAFT COULD NOT PRESSURIZE IN AUTO/MANUAL OR STANDBY. FLEW AT 10,000 MSL UNPRESSURIZED, REQUIRED FUEL STOP IN MCI. REMOVED AND REPLACED LEFT HAND PACK SHUTOFF VALVE, OPS CHECKED OK.Jan 31, 1996 · N727DH · Boeing 727228 · Cabin Cooling SystemSDR DHLA720007Switch · failedDURING CLIMB, FLAPS UP LEADING EDGE LIGHT INTERMITTENTLY ON. DURING FLAP EXTENSION, NR 2 L/E FLAP DID NOT LOCK UP. YELLOW AND GREEN L/E FLAP LIGHTS ON FORWARD PANEL WERE ALTERNATING. CHRISTMAS TREE INDICATED INTERMITTENT YELLOW LIGHT FOR NR 2 L/E FLAP. AT Jan 9, 1996 · N720DH · Boeing 727228 · Leading Edge Slat Control SystemSDR DHL95724010Press Indicator · failedON DESCENT, HYDRAULIC BRAKE PRESSURE INDICATED 2000 PSI. REMOVED AND REPLACED HYDRAULIC BRAKE ACCESSORY, BRAKE ACCUMULATOR PRESSURE TRANSMITTER AND HYDRAULIC BRAKE PRESSURE GAGE. MM 32-40.Nov 21, 1995 · N724DH · Boeing 727228 · Landing Gear Brake SystemSDR DHL95720005Engine · overtempDURING ROTATION, NR 1 EGT WENT INTO RED, PULLED THRUST LEVER BACK TO 1.85 EPR TO KEEP EGT OUT OF RED. REMOVED AND REPLACED NR 1 ENGINE IAW MM 71-00.Oct 5, 1995 · N720DH · Boeing 727228 · Engine (Turbine/Turboprop)SDR DHL9572408Indication · malfunctionedDURING EXTENSION FLAPS 2 BOTH INBOARD AND LEFT OUTBOARD WERE OUT OF INDICES ON FLAP GAUGE. SWAPPED FLAP INDICATORS FOR TROUBLESHOOTING. RAN FLAPS UP AND DOWN UNABLE TO FIND ANY TROUBLE, IAW MM 27-52-0A.Sep 10, 1995 · N724DH · Boeing 727228 · Trailing Flap Position Indicating SystemSDR 96ZZZM559Support Beam · crackedDURING D-CHECK, FOUND MAIN CABIN STATION 1183 LBL 35 VERTICAL SUPPORT BEAM IS CRACKED 28 INCHES ABOVE FLOOR AT ATTACH BOLTS. STOP DRILLED CRACK AS PER SRM 51-10-1. INSTALLED REPAIR AS PER DRAWING 65C34406 AT STATION 1183 LBL 35 FROM WL 23 TO WL 242.Sep 7, 1995 · N727DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR DHL9572405Mechanism · lack of lubeMAIN CARGO DOOR LIGHT ON DOOR ANNUNCIATOR PANEL ILLUMINATED AT FL 290. CARGO UNLOCK LIGHT ILLUMINATED ACCOMPANIED BY LOUD THUNK THAT WAS HEARD AND FELT. FOUND FASTENERS LOOSE AT TORQUE TUBE/ACTUATOR BRACKET ON LATCHES 6 AND 7, RESECURED, ADJUSTED AND LUBED. Sep 6, 1995 · N724DH · Boeing 727228 · Cargo/Baggage DoorsSDR DHLA9572005Epr Gauge · malfunctionedDURING TAKEOFF ROLL, LOST NR 1 EPR INDICATION, ALL OTHER PARAMETERS NORMAL. RECEIVED AUTO PACK TRIP, ABORTED TAKEOFF. RAN NR 1 ENGINE TO TAKEOFF POWER, ALL INDICATONS NORMAL. RESUMED SCHEDULED FLIGHT PLAN.Aug 4, 1995 · N720DH · Boeing 727228 · Engine Pressure Ratio (EPR)SDR DHL95727002Oil Cap · missingDURING CLIMB, NR 2 ENGINE OIL QTY DROPPED FROM 4 GALLONS TO 1.5 GALLONS WITH OIL TEMPERATURE CLIMBING. PERFORMED AIR TURNBACK, LANDED WITHOUT INCIDENT. INSTALLED CAP AND SERVICED OIL.Jul 11, 1995 · N727DH · Boeing 727228 · Turbine Engine Oil SystemSDR 96ZZZM602Floor Beam · corrodedDURING D-CHECK, FORWARD CARGO COMPARTMENT FLOOR BEAMS HAVE ANCHOR NUTS CORRODED AND CORROSION UNDER ANCHOR NUTS FROM LEFT AND RIGHT LINER ATTACH WEB AT STATION 716. CUT DAMAGE AREA AS PER SRM 53-10-8 AND INSTALLED REPAIR AS PER SRM 53-10-8, 51-30-2 AND 51-40-Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Main, Floor BeamSDR 96ZZZM601Floor Beam · corrodedDURING D-CHECK, FOUND FLOOR BEAM TOP FLANGE RBL 42 TO RBL 64 STATION 380 HAS CORROSION. CUT OUT DAMAGED AREA OF FLOOR BEAM BS 380 LBL 52 10 INCHES APPROX CLEANED AREA, NO MORE CORROSION FOUND. TREATED AND PRIMED PER SRM 51-10-2. INSTALLED FLOOR BEAM REPAIR Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Main, Floor BeamSDR 96ZZZM600Floor Support · damagedDURING D-CHECK, FOUND STATION 400 FLOOR BEAM APPROX RBL 60 HAS HOLE IN TOP CHORD TO CLOSE TO EDGE, BAD E/D. CUT OUT DAMAGE SECTION UPPER CHORD PER SRM 53-108. INSTALLED UPPER FLOOR BEAM REPAIR PER SRM 53-10-8 3 INCH BY 8 INCH.Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Miscellaneous StructureSDR 96ZZZM599Angle · corrodedDURING D-CHECK, FOUND BETWEEN STATION 480 AND 500 LEFT SIDE ANGLE AT LBL 62, CORROSION. REMOVED CORROSION LEFT SIDE STATION 480 TO 460 .001 MATERIAL LOSS PER SRM 51-10-6. REMOVED 20 INCH 7075-T6 511 A200/U PER SRM 51-10-1 PAR 4. INSTALLED NEW ANGLE 20 INCH Jul 9, 1995 · N727DH · Boeing 727228 · Fuselage Miscellaneous Structure
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